AD/BEECH 56/26 - Emergency Exits - Placards and Markings

Overview

The Civil Aviation Regulations 1998 were enacted to regulate civil aviation in Australia, ensuring safety and efficiency in the aviation industry. Specifically, Part 39, Section 105 of these Regulations includes Airworthiness Directives that address safety concerns through mandatory compliance. One such directive is AD/BEECH 56/26, which concerns the Beechcraft 56TC (Turbo Baron) series aeroplanes, aiming to standardise emergency exit placards and modify the openable window latch. This directive was introduced to address potential safety issues related to emergency exits and window latches in these aircraft models, thereby enhancing overall safety. The directive requires compliance within 100 hours of time in service after 31 January 1984 or at the next scheduled inspection, ensuring that these critical safety measures are promptly implemented. The Civil Aviation Safety Authority, under the authority of the Australian Parliament, enacts these regulations to maintain high safety standards in civil aviation.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all Beechcraft 56TC (Turbo Baron) series aeroplanes with serial numbers referenced in Beechcraft Service Instruction No. 1241. This regulation mandates adherence to the Airworthiness Directive AD/BEECH 56/26 concerning emergency exit placards and the modification of the openable window latch to ensure compliance with safety standards. The directive applies to all operators of the specified aircraft models and requires action in accordance with the outlined Beechcraft Service Instruction. Compliance must be achieved within 100 hours of the aircraft being in service after 31 January 1984, or at the next scheduled inspection for Maintenance Release issue after this date, whichever is later. This regulation operates under the jurisdiction of the Commonwealth of Australia and is enforced by the Civil Aviation Safety Authority (CASA). There are no stated exclusions or exemptions, and any further application details or amendments are addressed through subordinate instruments issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998, particularly under Part 39, impose specific directives regarding the airworthiness of certain aircraft models. In this context, the regulation AD/BEECH 56/26 pertains to Beechcraft 56TC (Turbo Baron) Series aeroplanes, focusing on emergency exits, placards, and markings (section 1/84). The regulation is applicable to all models with serial numbers referenced in Beechcraft Service Instruction No. 1241. To meet these requirements, operators must ensure that the actions specified in Beechcraft Service Instruction No. 1241 are implemented. The main obligation imposed by this directive is that compliance must be achieved within 100 hours of time in service following 31 January 1984, or at the next scheduled inspection for Maintenance Release issue after the same date, whichever is later. This stipulation underscores the importance of timely adherence to the specified modifications, ensuring that all safety standards are met promptly. Should an operator fail to comply with these directives, there could be significant consequences. While specific penalties are not detailed in the legislative instrument, non-compliance with Civil Aviation Regulations can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). These actions could include fines, suspension of operations, or other regulatory penalties. Such consequences are intended to enforce strict adherence to safety protocols and maintain the high standards of airworthiness required in civil aviation.